{"projectId":14573,"project":{"projectId":14573,"title":"Onboard Optical Navigation Measurement Processing in GEONS","startDate":"2013-10-01","startYear":2013,"startMonth":10,"endDate":"2016-09-01","endYear":2016,"endMonth":9,"programId":153,"program":{"ableToSelect":false,"acronym":"GSFC IRAD","isActive":true,"description":"<p>Goddard&#39;s IRAD program is managed under Goddard&#39;s Office of Chief Technologist.&nbsp; Activities are coordinated in collaboration with the Sciences and Exploration Directorate; Applied Engineering and Technology Directorate; Flight Projects Directorate; Wallops Flight Facility; New Opportunites Office; SBIR/STTR program; Goddard Strategic Partnerships Office; and the Export Compliance Office.</p><p>IRAD provides&quot;seed funding&quot; to develop concepts, reduce technology risk, and advance human capital and technological capabilities.&nbsp; The program is highly competitive, opportunity-driven, and 100% strategically aligned with NASA&#39;s and GSFC&#39;s strategic priorities.&nbsp; A significant portion of the program is focused on Early Stage Innovations for high-risk, strategically aligned, potential high-payoff technologies that are longer-term or lower TRL.</p>","parentProgram":{"ableToSelect":false,"acronym":"IRAD","isActive":true,"programId":87,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Center Independent Research & Development","acronymOrTitle":"IRAD"},"parentProgramId":87,"programId":153,"responsibleMd":{"organizationId":4910,"organizationName":"Mission Support Directorate","acronym":"MSD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4910,"title":"Center Independent Research & Development: GSFC IRAD","acronymOrTitle":"GSFC IRAD"},"description":"<p>Optical Navigation (OpNav) measurements derived from spacecraft-based images are a powerful data type in the precision orbit determination process. &nbsp;OpNav measurements are an enabling data type for small body proximity operations and are required to successfully navigate a spacecraft in the vicinity of asteroids, comets, and planetary satellites.&nbsp; Furthermore, onboard OpNav measurement processing and autonomous navigation have operational advantages compared to traditional ground-in-the-loop orbit determination.&nbsp; Therefore, NASA has a strategic interest in developing in-house OpNav data processing for onboard autonomous navigation.</p><p>The purpose of this IRAD is to develop in-house OpNav software tools and expertise to support the next generation of interplanetary and small body missions.&nbsp; Upon completion of this development effort, current onboard navigation software (GEONS) will be enhanced to use high-fidelity camera models for optical navigation measurement processing.</p> <p>The objective of this IRAD is to establish in-house onboard OpNav measurement data processing capabilities through software development and testing.&nbsp; Software development will include: 1) celestial and terrain-relative OpNav data processing, 2) high-fidelity camera modeling, and 3) onboard orbit determination software integration and testing.</p><p>Upon successful completion of this IRAD, enhancements to the Goddard Enhanced Onboard Navigation System (GEONS) will allow onboard orbit determination using optical navigation image data for interplanetary and small body spacecraft operations.&nbsp; GEONS will ingest and process celestial and terrain-relative OpNav data in the form of control points (pixel/line) located in an image.&nbsp; The processed measurements are then used to supplement radiometric data in the onboard orbit determination solution and produce real-time estimates of the spacecraft&rsquo;s position and velocity relative to the target body.&nbsp; The resulting navigation solutions will enable near-real time control, maneuver planning, and hazard avoidance for complex proximity operations.&nbsp; GEONS was chosen as the target platform because of its high heritage and operational use as an onboard spacecraft navigation system.</p>","benefits":"<p>Supplementing current onboard navigation software with OpNav data processing capabilities will better position NASA to execute future missions to asteroids, comets, and planetary satellites.&nbsp; Future small body mission opportunities include Discovery-class science missions, robotic precursors and captures for human near-Earth asteroid (NEA) missions, and the human NEA missions themselves.&nbsp; The most recent Planetary Decadal Survey specifically highlights mission opportunities to small bodies, including asteroid and comet sample return missions, and precision touchdown on a planetary surface.&nbsp; Furthermore, the experience gained and software developed with this IRAD will support future development efforts for the next generation of autonomous navigation systems, including autonomous rendezvous and docking systems for spacecraft servicing applications.</p>","releaseStatus":"Released","status":"Completed","viewCount":704,"destinationType":[],"trlBegin":3,"trlCurrent":3,"trlEnd":5,"lastUpdated":"01/08/20","favorited":false,"detailedFunding":false,"projectContacts":[{"contactId":118939,"canUserEdit":false,"firstName":"Dennis","lastName":"Woodfork","fullName":"Dennis W Woodfork","fullNameInverted":"Woodfork, Dennis W","middleInitial":"W","email":"dennis.w.woodfork@nasa.gov","receiveEmail":"Subscribed_User","projectContactRole":"Project_Manager","projectContactId":11556,"projectId":14573,"programContactRolePretty":"","projectContactRolePretty":"Project Manager"},{"contactId":83618,"canUserEdit":false,"firstName":"Cinnamon","lastName":"Wright","fullName":"Cinnamon A Wright","fullNameInverted":"Wright, Cinnamon 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navigation, inertial navigation (translation) filter, inertial attitude estimation filter, ascent vehicle filter, Earth-independent deep space navigation, celestial navigation, landmark navigation, X-ray pulsar navigation, vehicle-relative navigation (translation) filter, vehicle-relative attitude filter, swarm navigation, angles-only navigation, double line of sight navigation, small body prox ops and landing filter","level":3,"hasChildren":false,"selected":false,"isPrimary":true,"hasInteriorContent":true},"primaryTxTree":[[{"taxonomyNodeId":11464,"taxonomyRootId":8817,"code":"TX17","title":"GN&C","level":1,"hasChildren":true,"selected":false,"hasInteriorContent":true},{"taxonomyNodeId":11468,"taxonomyRootId":8817,"parentNodeId":11464,"code":"TX17.2","title":"Navigation Technologies","description":"Navigation technologies primarily consist of the robust, reliable, and computationally efficient mathematical algorithms and their associated software implementations for the functions of 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